Crash of a Learjet U-36A at Iwakuni AFB: 4 killed

Date & Time: May 21, 2003 at 1125 LT
Type of aircraft:
Operator:
Registration:
9202
Flight Type:
Survivors:
No
Schedule:
Iwakuni - Iwakuni
MSN:
36-056
YOM:
1988
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The crew departed Iwakuni AFB at 0900LT on a training mission over the Sea of Japan. At 1045LT, the aircraft returned to Iwakuni and the crew completed several touch-and-go manoeuvres on runway 02. During one of these procedures, the aircraft went out of control upon touchdown and crashed beside the runway, bursting into flames. All four crew members were killed.

Crash of a Dassault Falcon 20C in Toledo: 3 killed

Date & Time: Apr 8, 2003 at 1349 LT
Type of aircraft:
Operator:
Registration:
N183GA
Flight Type:
Survivors:
No
Schedule:
Traverse City – Toledo
MSN:
147
YOM:
1968
Flight number:
GAE183
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
4829
Captain / Total hours on type:
1100.00
Copilot / Total flying hours:
4632
Copilot / Total hours on type:
16
Aircraft flight hours:
19093
Circumstances:
The flight crew of the Fan Jet Falcon (DA-20) were practicing ILS approaches in instrument meteorological conditions with low clouds and rime ice. A first officer (FO) in training occupied the right seat, while the pilot-in-command (PIC), who was also the company chief pilot/check airman/designated flight instructor, occupied the left seat and was handling the radios. On the second approach, the airplane struck trees and burned, 1.57 nm from approach end of the runway. The landing gear was found extended, and the trailing edge and droop leading edge flaps were retracted. The wing and engine cowl anti-ice valves were found closed, consistent with it being off in the cockpit. Radar data revealed that on approach, the airspeed decreased from 188 knots to 141 knots at the outer marker, and continued to decrease down to 106 knots, when the airplane entered an abrupt descent and disappeared from radar. Simulator flights matched the radar profile with a flight idle approach, a power reduction inside the outer marker, and 1/4 inch of ice on the wings. In the simulator, the airplane stalled about 2 miles from the end of the runway with an airspeed of 103 kts. At flight idle, the engine power in the last 2 minutes of approach was below the recommended power setting for wing or engine anti-ice to be effective. Vref and stall speeds were computed to be 129 kts and 96 kts, with wing flaps and droop leading edges retracted. The PIC had about 1,100 hours in the make and model. The PIC did not have any documented previous flight instruction experience in make and model or any other multi-engine airplanes. The PIC had given 4 pilot proficiency checks in the DA-20 since receiving his check airman designation. The company Director of Operations reported that the accident FO was the first student the PIC had taken through the initial second-in-command course. The PIC and FO had received all of their turbojet experience with the operator.
Probable cause:
The flight instructor's inadequate supervision of the flight, including his failure to maintain an approach airspeed consistent with the airplane's configuration, which resulted in an aerodynamic stall due to slow airspeed, and subsequent uncontrolled descent into trees. Factors were the icing conditions, the flight instructors failure to turn on the wing and engine anti-ice, and his lack of experience as an instructor pilot in the airplane.
Final Report:

Crash of a Cessna 421C Golden Eagle III in Humberside: 1 killed

Date & Time: Mar 29, 2003 at 1229 LT
Registration:
G-SAIR
Flight Type:
Survivors:
Yes
Schedule:
Humberside - Humberside
MSN:
421C-0471
YOM:
1978
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2250
Captain / Total hours on type:
1850.00
Copilot / Total flying hours:
20000
Copilot / Total hours on type:
600
Circumstances:
About 50 minutes into the flight, the aircraft returned to Humberside circuit and was cleared by ATC for a touch-and-go landing on Runway 21. The landing was firm but otherwise uneventful and witnesses heard the power being applied as it accelerated for takeoff. Just before rotation two large "puffs of smoke" were seen to come from the vicinity of the mainwheels as both propellers struck the runway. The aircraft then lifted off and almost immediately began to yaw and roll to the left. The left bank reached an estimated maximum of 90° but reduced just before the left wing tip struck the ground. The aircraft then cartwheeled across the grass to the south of the runway and burst into flames. The owner in the left pilot's seat and the pilot in the right pilot's seat escaped from the wreckage, but the flight examiner, who was occupying a seat in the passenger cabin, was unable to vacate the aircraft and subsequently died of injuries sustained in the post impact fire. An engineering investigation found no fault with the aircraft that might have caused the accident. The investigation concluded that the most probable cause was an inadvertent retraction of the landing gear whilst the aircraft was still on the ground.
Probable cause:
An engineering investigation found no fault with the aircraft that might have caused the accident. The investigation concluded that the most probable cause was an inadvertent retraction of the landing gear whilst the aircraft was still on the ground. The confusion over individual roles would have been resolved if the examiner had given a pre-flight briefing in line with the guidance contained in the FAA Designated Examiners' Handbook, but both pilots have stated that this briefing did not take place. In any event, the FAA Handbook and FARs are unclear on who should be the commander of the flight although FAR 61.47 states the examiner is not normally to be the Pilot in Command except by prior agreement with the applicant or other person who would normally be acting as Pilot in Command. Nevertheless, it is clear that the instructor should have been briefed that he was fulfilling the safety pilot role and was responsible for "protect(ing) the overall safety of the flight to whatever extent is necessary". If the instructor had clearly understood this responsibility, he might have monitored the owner's actions more closely during the touch-and-go and might have intervened earlier. Notwithstanding the confusion, the instructor took control when he considered that the owner was not taking appropriate action to control the aircraft, although the actual moment that he took control is in dispute. Given the owner's belief that the instructor was the commander and that the instructor was in any case by far the more experienced pilot, it is not surprising that he relinquished control even though, unknowingly, he had a more complete understanding of the aircraft's predicament. The flight time from the propeller strikes to the next ground impact was only a few seconds. Once the aircraft became airborne with a significant amount of power applied and a badly damaged left propeller, the situation was well beyond any emergency for which either pilot might have trained. The options for action were very limited and would have required a full appreciation of the circumstances, plus extremely rapid analysis and reactions if those actions were to be successful.
Final Report:

Crash of a Canadair CL-215-6B11 off Port de Pollença: 2 killed

Date & Time: Mar 25, 2003
Type of aircraft:
Operator:
Registration:
UD.13-29
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
1124
YOM:
1990
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew was completing a training flight consisting of dropping survival equipment when the aircraft crashed in unknown circumstances in the sea off Port de Pollença. Two crew members were rescued while two others were killed.

Ground accident of a Fokker F27 Friendship 500 in Blenheim

Date & Time: Feb 27, 2003 at 1950 LT
Type of aircraft:
Operator:
Registration:
ZK-NAN
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Blenheim - Blenheim
MSN:
10365
YOM:
1968
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The Airwork F-27 was on a training flight, during which the crew carried out an exercise that simulated a gear problem. They extended the gear using the emergency system. However, after landing they did not select the main gear handle down and in addition did not install the gear locking pins. The crew were then distracted by other events and during this the co-pilot selected the emergency gear handle up to reset the system. The main gear then partially collapsed.

Ground accident of a Dornier DO228-201 in Karachi

Date & Time: Feb 19, 2003
Type of aircraft:
Operator:
Registration:
AP-BGF
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Karachi - Karachi
MSN:
8016
YOM:
1983
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful training flight at Karachi-Quaid-e-Azam Airport, the crew was taxiing to his parking place when control was lost. The aircraft rolled across the apron and eventually collided with a concrete wall. Both pilots escaped uninjured while the aircraft was damaged beyond repair.

Crash of a Britten-Norman BN-2A-21 Defender at Braasschaat AFB

Date & Time: Feb 14, 2003
Type of aircraft:
Operator:
Registration:
B-03
Flight Type:
Survivors:
Yes
Schedule:
Braasschaat - Braasschaat
MSN:
476
YOM:
1975
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a local training flight at Braasschaat AFB. For unknown reasons, the twin engine aircraft landed hard and bounced several times before coming to rest on the runway. Both pilots escaped with minor injuries and the aircraft was damaged beyond repair.

Crash of a Cessna 208B Super Cargomaster in San Angelo

Date & Time: Jan 24, 2003 at 1015 LT
Type of aircraft:
Operator:
Registration:
N944FE
Flight Type:
Survivors:
Yes
Schedule:
San Angelo - San Angelo
MSN:
208B-0044
YOM:
1987
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4356
Copilot / Total flying hours:
13884
Aircraft flight hours:
7503
Circumstances:
The airplane impacted a dirt field and a power line following a loss of control during a simulated engine failure while on a Part 135 proficiency check flight. Both pilots were seriously injured and could not recall any details of the flight after the simulated engine failure. Witnesses observed the airplane flying on a westerly heading at an altitude of 100 to 200 feet, and descending. They heard the sound of an engine “surging” and observed the airplane’s wings bank left and right. The airplane continued to descend and impacted the ground and power lines before becoming inverted. A pilot-rated witness reported that he observed about ¼ inch of clear and rime ice on the airplane’s protected surfaces (deice boots) and about ½ inch of ice on the airplane’s unprotected surfaces. An NTSB performance study of the accident flight based on radar data indicated that the airplane entered a descent rate of 1,300 feet per minute (fpm) about 1,100 feet above the ground. This rate of descent was associated with a decrease in airspeed from 130 knots to 92 knots over a span of 30 seconds. The airplane’s rate of descent leveled off at the 1,300 fpm rate for 45 seconds before increasing to a 2,000 fpm descent rate. The true airspeed fluctuated between a low of 88 knots to 102 knots during the last 45 seconds of flight. According to the aircraft manufacturer, the clean, wing flaps up stall speed was 78 knots. However, after a light rime encounter, the Pilot’s Operating Handbook (POH) instructed pilots to maintain additional airspeed (10 to 20 KIAS) on approach “to compensate for the increased pre-stall buffet associated with ice on the unprotected areas and the increased weight.” With flaps up, a minimum approach speed of 105 KIAS was recommended. The POH also stated that a significantly higher airspeed should be maintained if ½ inch of clear ice had accumulated on the wings.
Probable cause:
The flight crew's failure to cycle the deice boots prior to conducting a simulated forced landing and their failure to maintain adequate airspeed during the maneuver, which resulted in an inadvertent stall and subsequent loss of control. A contributing factor was the ice accumulation on the leading edges of the airfoils.
Final Report:

Crash of a Lockheed MC-130H Hercules in Caguas: 10 killed

Date & Time: Aug 7, 2002 at 2050 LT
Type of aircraft:
Operator:
Registration:
90-0161
Flight Type:
Survivors:
No
Site:
Schedule:
Roosevelt Roads - Roosevelt Roads
MSN:
5265
YOM:
1991
Country:
Crew on board:
10
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
10
Circumstances:
The crew departed Roosevelt Roads NAS on a local training flight. In the evening, while returning the to NAS, the crew encountered poor weather conditions with low clouds, limited visibility and rain falls. While descending at low height, the crew suffered a loss of situational awareness and failed to respond to obstacle warnings. The four engine aircraft collided with trees and crashed on the top of Mt Perucho. The aircraft disintegrated on impact and all 10 crew members were killed.
Probable cause:
By clear and convincing evidence, the cause of this mishap was an uncharacteristic loss of situational awareness by the entire mishap flight deck crew and the subsequent lack of an appropriate response to obstacle warnings. The Board President further found the following factors substantially contributed to the mishap: overall crew preparation, a misdirected focus on the weather, crew resource management dynamics, and crew judgment as it relates to existing directives.

Crash of a De Havilland DHC-5 Buffalo near Mugumo

Date & Time: Jul 25, 2002
Type of aircraft:
Operator:
Flight Phase:
Flight Type:
Survivors:
Yes
Location:
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was engaged in a training mission when the crew encountered engine problems. The aircraft crash landed near Mugumo and was damaged beyond repair. All seven occupants escaped uninjured.
Probable cause:
Engine failure for unknown reasons.